| Featured Space and Satellite Products |
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| Electronically Steerable Ka-Band Satellite Terminal | |
Satellite Terminal
from Get SAT
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| The Sling Blade SOLO LM Ka from Get SAT is an electronically steerable Ka-band satellite communication terminal engineered for land and maritime applications. Built on a flat-panel, phased-array architecture with no moving parts, the terminal enables rapid deployment and reliable connectivity while minimizing maintenance requirements. It operates across a transmit frequency range of 27.5–31 GHz and a receive frequency range of 17.7–21.2 GHz, supporting full 360° azimuth coverage with electronic beam steering from 15-90° elevation. |
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| 2800–8000 MHz Space Qualified RF Mixer | |
Space Qualified RF Mixer
from Mini Circuits
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| The MAC-80H+ from Mini-Circuits is a Space-Qualified, Hermetically Sealed RF Mixer engineered for high-reliability microwave frequency conversion. Operating over an RF and LO frequency range of 2800 to 8000 MHz and supporting an IF frequency range from DC to 1250 MHz, it enables flexible upconversion and downconversion across broadband satellite communication and radar systems. This mixer delivers a typical conversion loss of 6.0 dB from 2800–5000 MHz and 6.5 dB from 5000–8000 MHz, ensuring low and flat loss performance across the band. |
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| 8–18 GHz Rectangular Waveguide Circulator | |
Space Qualified Circulator
from Scientific Microwave Corporation
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| The SMC-020D750 from Scientific Microwave Corporation is a high-performance rectangular waveguide circulator designed for broadband operation across the 8–18 GHz frequency range. Engineered to provide stable signal routing and source protection, it supports full-band operation with deep impedance matching for enhanced RF system reliability. This circulator delivers low insertion loss of 0.8 dB, isolation of 14 dB, and return loss of 14 dB, ensuring efficient power transfer and reduced reflected energy in high-frequency microwave assemblies. |
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| 32-38 µm Multilayer Piezo Actuator | |
Space Actuator
from Physik Instrumente
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| The P-887.91 from Physik Instrumente is a Multilayer Piezo Actuator designed for high-precision motion control and high-power operation in demanding environments. It delivers a nominal travel range of 32–38 µm at 120 V, with an operating voltage range of -20 to 120 V, enabling fine positioning with exceptional responsiveness. The actuator provides a blocked force of up to 950 N and features a high resonance frequency of 40 kHz, making it ideal for dynamic and high-speed actuation tasks. This multilayer actuator incorporates a compact 5 × 5 × 36 mm form factor. |
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| Flight-Proven Satellite Payload Adapter | |
Satellite Payload Adapter
from Redwire Space
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| The LoFF from Redwire Space is a flight-proven satellite payload adapter designed to support high-capacity rideshare missions and complex multi-manifest launch configurations. Purpose-built as a custom adapter solution, LoFF enables the secure integration and deployment of a large number of secondary payloads alongside a primary spacecraft, maximizing launch vehicle utilization while improving overall mission efficiency.This space-qualified payload adapter provides a robust mechanical interface capable of hosting multiple CubeSats and secondary satellites. |
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| Sponsored by Marki Microwave | | |
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| 27.5-30 GHz Output Block Downconverter | |
Low Noise Block
from GeoSync Microwave
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| The DBE3-28.75 from GeoSync Microwave is an outdoor Ka-band block downconverter designed for high-performance satellite communication ground systems. Accepting a wideband RF input across 27.5–30 GHz, it delivers three independent L-band IF outputs spanning 0.95-1.95 GHz, enabling efficient multi-transponder reception for advanced SATCOM architectures.This antenna-mounted downconverter features an LO frequency range of 9.75-10.65 GHz, providing stable frequency conversion with a gain of 30 dB. |
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| Space-Qualified LEO Microsatellite Platform | |
Satellite Bus & Platform
from Dhruva Space
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| The P-Nu from Dhruva Space is a space-qualified modular microsatellite bus engineered for Low Earth Orbit (LEO) missions, supporting spacecraft masses up to 500 kg. Designed with multi-payload accommodation capability, it enables flexible mission configurations for diverse commercial, scientific and defense applications. This platform features a 3-axis stabilized attitude control system to ensure precise payload alignment and high pointing performance for advanced mission requirements. It is delivered ready for payload integration. |
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| 12 V GPS Receiver for Space Applications | |
GNSS Receiver
from Berlin Space Technologies
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| The GPS-110 from Berlin Space Technologies is a space-qualified GPS receiver designed to deliver precise position, velocity, and timing solutions for satellite missions. Operating from a 12 V supply, it integrates dual GPS receivers within a dedicated computation unit, enabling reliable orbit determination and navigation support in Low Earth Orbit. This receiver provides position accuracy of 10 meters and velocity accuracy of 0.1 m/s, ensuring dependable orbital state estimation for spacecraft control systems. It achieves a timing accuracy of 20 ns and a time to first fix of 40 s. |
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| External Flight Test Platform (EFTP) | |
Satellite Bus & Platform
from Sidus Space
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| The EFTP Platform from Sidus Space is a space-qualified satellite bus and external flight test platform engineered to enable rapid on-orbit technology demonstration and validation. Operating with a 28 V bus voltage, it provides a versatile infrastructure for hosting experimental payloads and returning critical performance data from the space environment. Designed for accelerated deployment timelines of approximately 15 weeks, the platform supports detailed post-mission analysis of environmental effects encountered in orbit. |
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| Single-Stage Suborbital Launch Vehicle | |
Satellite Launch Vehicle Platform
from Skyrora Ltd
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| The Skylark L from Skyrora Ltd is a Single-Stage Suborbital Launch Vehicle designed to deliver research and technology demonstration payloads to altitudes exceeding 100 km. Powered by a high-test peroxide (HTP) and kerosene bipropellant propulsion system, this suborbital launch vehicle serves as a guided sounding rocket platform for microgravity experiments, atmospheric research, and flight qualification missions. With an overall length of 11.65 m and a diameter of 0.7 m, it has a lift-off mass of approximately 2,466 kg and supports payloads of up to 50 kg. |
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